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Design, simulation and evaluation of advanced display concepts for the F-16 control configured vehicleAdvanced display concepts to augment the tracking ability of the F-16 Control Configured Vehicle (CCV) were designed, simulated, and evaluated. A fixed-base simulator was modified to represent the F-16 CCV. An isometric sidearm control stick and two-axis CCV thumb button were installed in the cockpit. The forward cockpit CRT was programmed to present an external scene (numbered runway, horizon) and the designed Heads Up Display. The cockpit interior was modified to represent a fighter and the F-16 CCV dynamics and direct lift and side force modes were programmed. Compensatory displays were designed from man-machine considerations. Pilots evaluated the Heads up Display and compensatory displays during simulated descents in the presence of several levels of filtered, zero-mean winds gusts. During a descent from 2500 feet to the runway, the pilots tracked a point on the runway utilizing the basic F-16, F-16 CCV, and F-16 CCV with advanced displays. Substantial tracking improvements resulted utilizing the CCV modes, and the displays were found to even further enhance the tracking ability of the F-16 CCV.
Document ID
19820026186
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Klein, R. W.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Hollister, W. M.
(MIT)
Date Acquired
August 10, 2013
Publication Date
July 1, 1982
Publication Information
Publication: NASA. Ames Research Center 16th Ann. Conf. on Manual Control
Subject Category
Man/System Technology And Life Support
Accession Number
82N34062
Funding Number(s)
CONTRACT_GRANT: AF-AFOSR-3260-78
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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